Computer Science – Sound
Scientific paper
Jun 1989
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989esasp.291..209b&link_type=abstract
In ESA, European Rocket and Balloon Programs and Related Research p 209-212 (SEE N90-13826 05-42)
Computer Science
Sound
Brazilian Space Program, Launch Vehicle Configurations, Propulsion System Configurations, Sounding Rockets, Design Analysis, Feasibility Analysis, Launchers, Ranges (Facilities)
Scientific paper
The development of the Satellite Launcher Vehicle (SLV) is presented. In particular, the attention is focused on the acquisition of the propulsion parameters of the 4th stage propulsor. The device feasibility analysis is considered. The system consists of a two staged sounding rocket. Its second stage contains the SVL, which can be launched by the 4th stage propulsor to a height range of about 50 to 60 km.
Boscov Jayme
Toyama Wilson Katsumi
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